Transport Weight Reduction Through MDO: The Strut-Braced Wing Transonic Transport
Author:
Affiliation:
1. Avionics Specialties, Inc
2. AVID LLC
3. National Institute of Aerospace
4. University of Florida
5. Virginia Tech
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4667
Reference32 articles.
1. Hurel,M."TheAdvantagesofHighAspectRatios,"Interavia,VolumeVII,No.12,1952,pp.695-699.
2. Wing planforms for large military transports
3. Park, H. P. "The Effect on Block Fuel Consumption of a Strutted vs. Cantilever Wing for a Short Haul Transport Including StrutAeroelastic Considerations," AIAA-78-1454,LosAngeles, California, Aug. 21-23,1978
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